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Technology / Hall effect thruster / Plasma propulsion engine / Plasma / Electron / Langmuir probe / Ion / Ion thruster / Electrodeless plasma thruster / Spacecraft propulsion / Physics / Propulsion


Document Date: 2007-05-07 14:47:33

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City

Osaka / /

Company

Princeton Plasma Physics Laboratory / Plasma Dynamics Laboratory / /

Country

Germany / Korea / /

Currency

USD / /

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Facility

Princeton University / NASA Marshall Space Flight Center / American Institute of Physics Downloaded / Korean Advanced Institute of Science / Nathaniel J. Fisch Princeton University Plasma Physics Laboratory / American Institute of Physics / Plasma Dynamics Laboratory facility / Osaka University / Fisch port / /

IndustryTerm

gas flow / background gas / average energy / satellite orbit control / propulsion devices / crossover energy / electron energy losses / high-energy ions / ion energy distribution mea / conventional chemical rockets / high energy / ion energy distribution measurements / thermal energy / average ion energy leads / propellant gas atom / space applications / neutral gas density / propulsion device / low background gas pressure environment / energy sink / gas distributor / thruster technology / mature electric propulsion device / energy / ion energy distribution function / /

Organization

JapanÍ’25 and Korean Advanced Institute of Science and Technology / American Institute of Physics / Department of Mechanical / Princeton University / National Aeronautics and Space Administration / U.S. Securities and Exchange Commission / Yegeny Raitses / and Nathaniel J. Fisch Princeton University Plasma Physics Laboratory / Osaka University / /

Position

Invited speaker / /

ProvinceOrState

New Jersey / /

Technology

low-power Hall thruster technology / /

URL

http /

SocialTag